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    Gas turbine engines and methods associated therewith
    83.
    发明授权
    Gas turbine engines and methods associated therewith 有权

    公开(公告)号：US11585224B2

    公开(公告)日：2023-02-21

    申请号：US16987872

    申请日：2020-08-07

    Applicant: General Electric Company

    Inventor： Gregory Terrence Garay ,  Tingfan Pang ,  Daniel Endecott Osgood ,  Ryan Christopher Jones

    IPC: F01D5/14 ,  F01D25/12 ,  F23C7/02 ,  F01D25/14

    Abstract: A method of forming a gas turbine engine component, the method including forming a plurality of cooling apertures in a preform structure of the component, the plurality of cooling apertures of the preform structure comprising a first cooling aperture and a second cooling aperture, wherein cross-sectional shapes of the first and second cooling apertures of the preform structure are different from one another, as measured in a same relative plane; and applying a coating to at least a portion of the preform structure to form the component, wherein a cross-sectional shape of the first and second cooling apertures of the component are approximately the same as one another, as measured in the same relative plane.

    Turbine engine component and method of cooling
    85.
    发明授权
    Turbine engine component and method of cooling 有权

    公开(公告)号：US11499433B2

    公开(公告)日：2022-11-15

    申请号：US16223279

    申请日：2018-12-18

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Daniel Endecott Osgood ,  Zachary Daniel Webster

    IPC: F01D5/18 ,  F01D5/30

    Abstract: A turbine engine airfoil and method of cooling includes an outer wall defining an exterior surface bounding an interior and defining a pressure side and a suction side extending between a leading edge and a trailing edge to define a chord-wise direction and extending between a root and a tip to define a span-wise direction. The airfoil can also include at least one cooling conduit and an impingement zone located within the at least one cooling conduit.

    Engine component with cooling hole
    87.
    发明授权
    Engine component with cooling hole 有权

    公开(公告)号：US11359494B2

    公开(公告)日：2022-06-14

    申请号：US16532787

    申请日：2019-08-06

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Daniel Endecott Osgood ,  Kirk Douglas Gallier ,  Daniel Lee Durstock ,  Zachary Daniel Webster ,  Gregory Terrence Garay

    IPC: F01D5/18

    Abstract: An apparatus and method for an engine component for a turbine engine comprising an outer wall having an outer surface and bounding an interior, the outer wall defining a pressure side and a suction side, extending axially between a leading edge and a trailing edge to define a chord-wise direction, and extending radially between a root and a tip to define a span-wise direction, at least one cooling supply conduit provided in the interior, and at least one cooling passage fluidly coupling the at least one cooling supply conduit to the outer surface of the outer wall, the at least one cooling passage comprising an outlet opening onto the outer surface along the leading edge, an inlet fluidly coupled to the at least one cooling supply conduit, and a curved passage defining a curvilinear centerline.

    Monitoring system for a gas turbine engine
    90.
    发明授权
    Monitoring system for a gas turbine engine 有权

    公开(公告)号：US11199105B2

    公开(公告)日：2021-12-14

    申请号：US15660608

    申请日：2017-07-26

    Applicant: General Electric Company

    Inventor： Guanghua Wang ,  Daniel Endecott Osgood ,  William Stewart ,  Jason Edward Dees ,  Eric John Ruggiero

    IPC: F01D21/00 ,  G06T7/00 ,  H04N5/33

    Abstract: An optical monitoring system includes a controller configured to determine a predicted status of a component based on an operational time of a rotary machine and an individual model. The controller is also configured to receive a first signal indicative of an infrared spectrum image of the component from one or more cameras. Further, the controller is configured to determine a current status of the component based on the first signal and compare the current status to the predicted status of the component. Additionally, the controller is configured to update the predicted status of the component such that the predicted status matches the current status of the component and update at least one parameter of the individual model of the component based on the comparison.

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